TITAN 3C TRANSTAGE R/B, 9855
Orbit data source: Space-Track
TITAN 3C TRANSTAGE R/B, 9855 is space debris in GEO originally from a launch on Sun, 06 Feb 1977 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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9855 intel report (Beta)
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Edit Public Description
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TLE from 1 day ago
0 TITAN 3C TRANSTAGE R/B
1 09855U 77007C 25198.28989870 .00000061 00000-0 00000-0 0 9991
2 09855 4.2584 273.3992 0015543 36.5698 323.7503 1.00214361 22007
Epoch: 2025-07-17T06:57Z
TLE epoch observation values (Epoch: 2025-07-17T06:57:27.247Z)
Latitude
0.00001°
Longitude
-126.10544°
Altitude
35,749.099 km
Speed
3.078 km/s
True Right ascension
18h 14m 27s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
0.66482°
Longitude
-117.12921°
Altitude
35,743.539 km
Speed
3.078 km/s
Apparent Right ascension
18h 39m 33s
Apparent Declination
-5° 26' 38"
Sunlit
Visualization observer readout
Local Sidereal Time
20:15:09
Azimuth
211.553° SW
Elevation
39.582°
Doppler factor
1
Orbital elements
Apogee altitude
35,869.325 km
Perigee altitude
35,738.199 km
Semi-major axis
42,181.899 km
Eccentricity
0.00155
Inclination
4.2584°
RAAN
273.3992°
Arg. of periapsis
36.5698°
True anomaly
323.64482°
Mean anomaly
323.7503°
Eccentric anomaly
323.69758°
Mean motion
0.25053 °/min
Orbital period
1,436.97 mins
BSTAR
0
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Other satellites on launch #7 in the year 1977 (1977-02-06 UTC)
TITAN 3C TRANSTAGE R/B Visibility forecast
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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1440 mins | 2025-07-18 07:30:10.273Z | 211.542° SW | 2025-07-18 13:02:10.273Z | 213.454° SW | 34.442° | 2025-07-19 07:30:10.273Z | 211.844° SW |
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9855 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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